Method for assisting a pilot in controlling an aircraft, assistance system for an aircraft pilot, and aircraft

A method for assisting a pilot in controlling an aircraft, an assistance system for an aircraft pilot, and an aircraft are disclosed herein. In one example, a method is disclosed of assisting a pilot in controlling an aircraft having a plurality of lift-generating propulsion devices. The method having steps that include, calculation of momentary control limitations for each control of the aircraft around a roll axis, a pitch axis, a yaw axis, and a total thrust T of the propulsion devices, and display of the calculated control limitations by a display device.